Author Details
Поршнев, В. А.
| Issue | Section | Title | File |
| Vol 8, No 3-1 (2009): Special Issue | AIRCRAFT AND SPACE ROCKET ENGINEERING | Agency of members of the pulse detonation engine on thrust characteristics |
 (Rus) |
| Vol 13, No 5-2 (2014): Special Issue | ISSUE WITHOUT SECTION | Rotary isochoric combustion chamber of a gas turbine engine |
(Rus) |
| Vol 13, No 5-2 (2014): Special Issue | ISSUE WITHOUT SECTION | Multicriterial choice of the best variant of the pulse detonation engine design for aircraft angular stabilization and orientation systems |
(Rus) |
| Vol 10, No 3-2 (2011): Special Issue | AIRCRAFT AND SPACE ROCKET ENGINEERING | Design procedure of fundamental parameters of the direct-flow detonation pulsing engine |
(Rus) |
| Vol 10, No 3-4 (2011): Special Issue | AIRCRAFT AND SPACE ROCKET ENGINEERING | Technique of conclusion the direct-flow detonation pulsing engine design to the leader position |
(Rus) |